US10473706B2ActiveUtilityA1

Optical sensing methods and systems for power applications, and the construction thereof

77
Assignee: HYPERION SENSORS INCPriority: Feb 15, 2016Filed: Feb 14, 2017Granted: Nov 12, 2019
Est. expiryFeb 15, 2036(~9.6 yrs left)· nominal 20-yr term from priority
G01K 11/32G01R 31/62G01K 1/14H01F 27/2871H01F 27/402H01F 27/323G01R 31/027
77
PatentIndex Score
2
Cited by
32
References
24
Claims

Abstract

Optical sensing methods and systems for power applications, and the construction thereof, are described herein. An example method of constructing a winding assembly includes mounting a sensing component to a coil former, and winding a coil onto the coil former so that the sensing component is positioned within the coil. A system and method for detecting operating conditions within a transformer using the described winding assemblies are described.

Claims

exact text as granted — not AI-modified
We claim: 
     
       1. A method of constructing a winding assembly, the method comprising:
 mounting a set of support spacers to a coil former with a plurality of the support spacers spaced circumferentially apart from each other about the coil former; 
 supporting a sensing component with at least the plurality of the support spacers; and 
 winding a coil onto the coil former, wherein the sensing component is positioned within the coil. 
 
     
     
       2. The method of  claim 1 , wherein:
 the sensing component comprises an optical fiber; and 
 supporting the sensing component comprises winding the optical fiber to the coil former. 
 
     
     
       3. The method of  claim 1 , wherein the coil comprises a set of primary coils and a set of secondary coils, the set of primary coils having a different number of turns than the set of secondary coils. 
     
     
       4. The method of  claim 1 , wherein the coil former comprises one of a former, a core, and a portion of the coil. 
     
     
       5. The method of  claim 4  comprises:
 providing the former as the coil former; and 
 mounting the sensing component to the former. 
 
     
     
       6. The method of  claim 4  comprises:
 providing the portion of the coil as the coil former; and 
 mounting the sensing component to the portion of the coil. 
 
     
     
       7. The method of  claim 1  comprises:
 defining a spacing in each support spacer for receiving a portion of the sensing component. 
 
     
     
       8. The method of  claim 7 , wherein the spacing is selected from the group consisting of a groove, slot and an opening. 
     
     
       9. The method of  claim 1  comprises:
 forming a plurality of ribs longitudinally on the coil former, wherein each rib in the plurality of ribs is spaced from each other; and 
 positioning the set of support spacers onto one or more ribs of the plurality of ribs. 
 
     
     
       10. The method of  claim 1  comprises:
 defining a plurality of slots on the coil former, wherein each slot is adapted to receive a support spacer of the set of support spacers; and 
 mounting the set of support spacers to one or more slots of the plurality of slots. 
 
     
     
       11. The method of  claim 1 , wherein winding the coil onto the coil former comprises:
 separating neighbouring turns within the coil with at least one spacer mounted to the coil former. 
 
     
     
       12. The method of  claim 6 , wherein winding the coil onto the coil former comprises:
 winding a remainder of the coil and the sensing component onto the portion of the coil acting as the coil former. 
 
     
     
       13. A winding assembly comprising:
 a set of support spacers mounted to a coil former with a plurality of the support spacers spaced circumferentially apart from each other about the coil former; 
 a sensing component supported with at least the plurality of the support spacers; and 
 a coil wound onto the coil former, wherein the sensing component is positioned within the coil. 
 
     
     
       14. The winding assembly of  claim 13 , wherein:
 neighbouring turns within the coil are separated with at least one spacer mounted to the coil former. 
 
     
     
       15. The winding assembly of  claim 13 , wherein:
 the sensing component comprises an optical fiber wound to the coil former. 
 
     
     
       16. The winding assembly of  claim 13 , wherein the coil comprises a set of primary coils and a set of secondary coils, the set of primary coils having a different number of turns than the set of secondary coils. 
     
     
       17. The winding assembly of  claim 13 , wherein the coil former comprises one of a former, a core, and a portion of the coil. 
     
     
       18. The winding assembly of  claim 17 , wherein:
 the sensing component is mounted to the former. 
 
     
     
       19. The winding assembly of  claim 17  wherein:
 the sensing component is mounted to the portion of the coil. 
 
     
     
       20. The winding assembly of  claim 13 , wherein:
 each support spacer is defined to have a spacing for receiving a portion of the sensing component. 
 
     
     
       21. The winding assembly of  claim 20 , wherein the spacing is selected from the group consisting of a groove, slot and an opening. 
     
     
       22. The winding assembly of  claim 13  comprises:
 a plurality of ribs formed longitudinally on the coil former, wherein each rib in the plurality of ribs is spaced from each other; and 
 the set of support spacers are positioned onto one or more ribs of the plurality of ribs. 
 
     
     
       23. The winding assembly of  claim 13  comprises:
 a plurality of slots defined on the coil former, wherein each slot is adapted to receive a support spacer of the set of support spacers; and 
 the set of support spacers is mounted to one or more slots of the plurality of slots. 
 
     
     
       24. The winding assembly of  claim 19 , wherein a remainder of the coil and the sensing component are wound onto the portion of the coil acting as the coil former.

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